Control of Nonlinear Spacecraft Attitude Motion
Completed by María Angélica Arroyo Bernal
November 23, 2017
31 hours (approximately)
María Angélica Arroyo Bernal's account is verified. Coursera certifies their successful completion of Control of Nonlinear Spacecraft Attitude Motion
What you will learn
Differentiate between a range of nonlinear stability concepts
Apply Lyapunov’s direct method to argue stability and convergence on a range of dynamical systems
Develop rate and attitude error measures for a 3-axis attitude control using Lyapunov theory
Analyze rigid body control convergence with unmodeled torque
Skills you will gain
- Category: Engineering Analysis
- Category: Control Systems
- Category: Torque (Physics)
